View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 39617U 26145.58840845 +.00000000 +00000-0 +00000-0 0 00009
2 39617 0.0539 320.4850 0002566 72.5631 85.4318 1.00270869 02
| Epoch (UTC): | 25 May 2026 14:07:18 |
| Eccentricity: | 0.0002566 |
| inclination: | 0.0539° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 320.4850° |
| argument of perigee: | 72.5631° |
| revolutions per day: | 1.00270869 |
| mean anomaly at epoch: | 85.4318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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